53902 | ИПУ РАН

Автор(ы):

Гулюкина С. И. (ИПУ РАН, Лаборатория 37)

Автор(ов):

Параметры публикации

Тип публикации:

Доклад

Название:

Aerodynamic Parameters Identification of the Nanosatellite TNS-0 No 2 to Enhance Ballistic Calculations Precision for Low-Flying Satellites

Электронная публикация:

Да

ISBN/ISSN:

978-1-7281-1730-0

DOI:

10.1109/MLSD.2019.8911071

Наименование конференции:

2019 12th International Conference "Management of Large-Scale System Development" (MLSD)

Наименование источника:

Proceedings of the 12th International Conference "Management of Large-Scale System Development" (MLSD)

Город:

Москва

Издательство:

IEEE

Год издания:

2019

Страницы:

1-4 https://ieeexplore.ieee.org/document/8911071

Аннотация

This report is devoted to an important problem of the space flight mechanics - the orbital motion analysis for the low-flying artificial Earth satellite with the goal to refine the parameters of the atmosphere to improve the prediction accuracy for the ballistic motion of orbital objects in the upper layers of the atmosphere.

Библиографическая ссылка:

Панкратов В.А., Гулюкина С.И. Aerodynamic Parameters Identification of the Nanosatellite TNS-0 No 2 to Enhance Ballistic Calculations Precision for Low-Flying Satellites / Proceedings of the 12th International Conference "Management of Large-Scale System Development" (MLSD). М.: IEEE, 2019. С. 1-4 https://ieeexplore.ieee.org/document/8911071.